FR3095191B1 - Système propulsif hybride et procédé de contrôle d’un tel système - Google Patents

Système propulsif hybride et procédé de contrôle d’un tel système Download PDF

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Publication number
FR3095191B1
FR3095191B1 FR1904034A FR1904034A FR3095191B1 FR 3095191 B1 FR3095191 B1 FR 3095191B1 FR 1904034 A FR1904034 A FR 1904034A FR 1904034 A FR1904034 A FR 1904034A FR 3095191 B1 FR3095191 B1 FR 3095191B1
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FR
France
Prior art keywords
electric
hybrid propulsion
conversion
control
rectifier
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1904034A
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English (en)
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FR3095191A1 (fr
Inventor
Loïs Pierre Denis Vive
Thomas Klonowski
Camel Serghine
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Helicopter Engines SAS
Original Assignee
Safran Helicopter Engines SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR1904034A priority Critical patent/FR3095191B1/fr
Application filed by Safran Helicopter Engines SAS filed Critical Safran Helicopter Engines SAS
Priority to CN202080031843.1A priority patent/CN113767048A/zh
Priority to PL20725789.0T priority patent/PL3956218T3/pl
Priority to US17/601,816 priority patent/US20220177147A1/en
Priority to CA3132945A priority patent/CA3132945A1/fr
Priority to PCT/FR2020/000116 priority patent/WO2020212656A1/fr
Priority to KR1020217034538A priority patent/KR20210151846A/ko
Priority to EP20725789.0A priority patent/EP3956218B1/fr
Priority to JP2021560271A priority patent/JP2022529612A/ja
Publication of FR3095191A1 publication Critical patent/FR3095191A1/fr
Application granted granted Critical
Publication of FR3095191B1 publication Critical patent/FR3095191B1/fr
Priority to IL287107A priority patent/IL287107A/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/026Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J3/00Circuit arrangements for ac mains or ac distribution networks
    • H02J3/36Arrangements for transfer of electric power between ac networks via a high-tension dc link
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00Electric power distribution systems onboard aircraft
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2310/00The network for supplying or distributing electric power characterised by its spatial reach or by the load
    • H02J2310/40The network being an on-board power network, i.e. within a vehicle
    • H02J2310/44The network being an on-board power network, i.e. within a vehicle for aircrafts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Power Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)

Abstract

L’invention concerne un système propulsif hybride (100) pour un aéronef à voilure tournante multi-rotors, comprenant : un moteur (112) à combustion interne, une machine électrique (114) accouplée au moteur à combustion interne, un redresseur (116) relié à la machine électrique, des moyens de conversion (118a, 188b, 188c, 118d), un réseau électrique (120) reliant le redresseur aux moyens de conversion, des moteurs électriques (122a, 122b, 122c, 122d) reliés aux moyens de conversion, des hélices (124a, 124b, 124c, 124d) accouplées aux moteurs électriques, Le système étant caractérisé en ce qu’il comprend : des moyens de détection configurés pour détecter une diminution d’une demande de puissance électrique au sein du système en dessous d’une valeur prédéterminée, des moyens de mise en court-circuit configurés pour court-circuiter la machine électrique lorsqu’une diminution de la demande de puissance électrique est détectée par les moyens de détection. Figure pour l'abrégé : Figure 4
FR1904034A 2019-04-16 2019-04-16 Système propulsif hybride et procédé de contrôle d’un tel système Active FR3095191B1 (fr)

Priority Applications (10)

Application Number Priority Date Filing Date Title
FR1904034A FR3095191B1 (fr) 2019-04-16 2019-04-16 Système propulsif hybride et procédé de contrôle d’un tel système
JP2021560271A JP2022529612A (ja) 2019-04-16 2020-04-10 ハイブリッド推進システムおよびそのようなシステムを制御するための方法
US17/601,816 US20220177147A1 (en) 2019-04-16 2020-04-10 Hybrid propulsion system and method for controlling such a system
CA3132945A CA3132945A1 (fr) 2019-04-16 2020-04-10 Systeme propulsif hybride et procede de controle d'un tel systeme
PCT/FR2020/000116 WO2020212656A1 (fr) 2019-04-16 2020-04-10 Système propulsif hybride et procédé de contrôle d'un tel système
KR1020217034538A KR20210151846A (ko) 2019-04-16 2020-04-10 하이브리드 추진 시스템 및 하이브리드 추진 시스템을 제어하는 방법
CN202080031843.1A CN113767048A (zh) 2019-04-16 2020-04-10 混合推进***和用于控制这种***的方法
PL20725789.0T PL3956218T3 (pl) 2019-04-16 2020-04-10 Hybrydowy układ napędowy i sposób sterowania takim układem
EP20725789.0A EP3956218B1 (fr) 2019-04-16 2020-04-10 Système propulsif hybride et procédé de contrôle d'un tel système
IL287107A IL287107A (en) 2019-04-16 2021-10-08 A hybrid propulsion system and a method for controlling such a system

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1904034 2019-04-16
FR1904034A FR3095191B1 (fr) 2019-04-16 2019-04-16 Système propulsif hybride et procédé de contrôle d’un tel système

Publications (2)

Publication Number Publication Date
FR3095191A1 FR3095191A1 (fr) 2020-10-23
FR3095191B1 true FR3095191B1 (fr) 2021-04-23

Family

ID=68072561

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1904034A Active FR3095191B1 (fr) 2019-04-16 2019-04-16 Système propulsif hybride et procédé de contrôle d’un tel système

Country Status (10)

Country Link
US (1) US20220177147A1 (fr)
EP (1) EP3956218B1 (fr)
JP (1) JP2022529612A (fr)
KR (1) KR20210151846A (fr)
CN (1) CN113767048A (fr)
CA (1) CA3132945A1 (fr)
FR (1) FR3095191B1 (fr)
IL (1) IL287107A (fr)
PL (1) PL3956218T3 (fr)
WO (1) WO2020212656A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11772807B2 (en) * 2020-06-18 2023-10-03 Textron Innovations Inc. Electric distributed anti-torque architecture
US20220135241A1 (en) * 2020-10-30 2022-05-05 Sonin Hybrid, LLC Systems and Methods for Controlling Torque for Aerial Vehicle
US11520361B2 (en) * 2021-02-17 2022-12-06 Rolls-Royce Singapore Pte. Ltd. Control for a target common bus voltage
JP2022157287A (ja) * 2021-03-31 2022-10-14 本田技研工業株式会社 電力供給システム
US20230166856A1 (en) * 2021-11-29 2023-06-01 General Electric Company System and method for electric load control for a vehicle
GB2613541A (en) * 2021-11-30 2023-06-14 Airbus Sas Shielding arrangement for aircraft wiring

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CZ382892A3 (en) * 1992-02-20 1993-09-15 Asea Brown Boveri Device with a gas turbine and method for starting thereof
JP2003189697A (ja) * 2001-12-19 2003-07-04 Kokusan Denki Co Ltd 交流発電機を備えた電源装置
EP1516424A2 (fr) * 2002-06-18 2005-03-23 Ingersoll-Rand Energy Systems Corporation Systeme de moteur a microturbine
CN101600882A (zh) * 2006-01-20 2009-12-09 西南风力公司 风力涡轮机的失速控制器以及触发条件的控制装置
DE102006045731A1 (de) * 2006-09-27 2008-04-03 Zf Friedrichshafen Ag Elektrodynamisches Antriebssystem
KR20080001344U (ko) * 2006-11-22 2008-05-27 (주)거화테크 소형 풍력발전기 자동과속 방지장치
GB2456179B (en) * 2008-01-07 2012-02-15 Converteam Technology Ltd Marine power distribution and propulsion systems
CN102889181B (zh) * 2011-01-21 2014-07-30 中科恒源科技股份有限公司 一种抗强风小型风力发电机
WO2013064928A1 (fr) * 2011-10-31 2013-05-10 Panacis Inc. Procédé et système pour arrêter automatiquement une turbine éolienne
US8810177B2 (en) * 2012-09-12 2014-08-19 GM Global Technology Operations LLC System and method for implementing a remedial electrical short
CN104791192B (zh) * 2015-04-16 2018-02-27 深圳市风光宝新能源科技有限公司 一种风力机限速与刹车保护控制的装置及方法
FR3056555B1 (fr) * 2016-09-29 2018-12-07 Safran Helicopter Engines Systeme propulsif hybride pour aeronef a voilure tournante multirotor comprenant des moyens ameliores de conversion dc/ac
WO2018175349A1 (fr) * 2017-03-19 2018-09-27 Zunum Aero, Inc. Aéronef hybride-électrique, et procédés, appareil et systèmes destinés à faciliter ledit aéronef
CN106877478B (zh) * 2017-04-28 2020-03-27 重庆三信电子股份有限公司 一种车用电源***及有源混合整流器和控制方法

Also Published As

Publication number Publication date
CA3132945A1 (fr) 2020-10-22
US20220177147A1 (en) 2022-06-09
PL3956218T3 (pl) 2023-12-11
EP3956218A1 (fr) 2022-02-23
CN113767048A (zh) 2021-12-07
WO2020212656A1 (fr) 2020-10-22
FR3095191A1 (fr) 2020-10-23
IL287107A (en) 2021-12-01
KR20210151846A (ko) 2021-12-14
EP3956218B1 (fr) 2023-08-30
JP2022529612A (ja) 2022-06-23

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